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- On the stability of the laminar mixing region between two parallel streams in a gas
- Creep-buckling analysis of rectangular-section columns
- Determination of boundary-layer transition Reynolds numbers by surface-temperature measurements of a 10 degree cone in various NACA supersonic wind tunnels
- The effect of longitudinal stiffeners located on one side of a plate on the compressive buckling stress of the plate-stiffener combination
- Analytical investigation of icing limit for diamond-shaped airfoil in transonic and supersonic flow
- Combined effect of damping screens and streams convergence on turbulence
- An analysis of statically indeterminate trusses having members stressed beyond the proportional limit
- Behavior in pure bending of a long monocoque beam of circular-arc cross section
- An analysis of normal-acceleration and airspeed data from a four-engine type of transport airplane in commercial operation on an eastern united states route from november 1947 to february 1950
- Combined-stress fatigue strength of 76S-T61 aluminum alloy with superimposed mean stresses and corrections for yielding
- Combustion instability in an acid-heptane rocket with a pressurized-gas propellant pumping system
- The compressible laminar boundary layer with heat transfer and small pressure gradient
- The effect of vertical chine strips on the planing characteristics of V- shaped prismatic surfaces having angles of dead rise of 20 degrees and 40 degrees
- Effect of processing variables on the transition temperature, strength, and ductility of high-purity, sintered, wrought molybdenum metal
- Effect of variation in rivet strength on the average stress at maximum load for aluminum-alloy, flat, z-stiffened compression panels that fail by local buckling
- Effect of type of porous surface and suction velocity distribution on the characteristics of a 10.5-percent-thick airfoil with area suction
- Experiments on mixed-free-and-forced-convective heat transfer connected with turbulent flow through a short tube
- Effect of prestraining of recrystallization temperature and mechanical properties of commercial, sintered, wrought molybdenum
- Evaluation of gust response characteristics of some existing aircraft with wing bending flexibility included
- Effects of symmetric and asymmetric thrust reversal on the aerodynamic characteristics of a model of a twin-engine airplane
- Estimated power reduction by water injection in a nonreturn supersonic wind tunnel
- An experimental investigation of secondary flow in an accelerating, rectangular elbow with 90 degrees of turning
- Experimental investigation of the effects of cooling on friction and on boundary-layer transition for low-speed gas flow at the entry of a tube
- Experimental investigation of the effect of rear-fuselage shape on ditching behavior
- Surveys of the flow fields at the propeller planes of six 40 degree sweptback wing-fuselage-nacelle combinations
- Summary of revised gust-velocity data obtained from V-G records taken on civil transport airplanes from 1933 to 1950
- Propeller-performance charts for transport airplanes
- Study of pressure effects on vaporization rate of drops in gas streams
- Studies of the use of Freon-12 as a wind tunnel testing medium
- Experimental stress analysis of stiffened cylinders with cutouts: Pure torsion
- Survey of portions of the iron-nickel-molybdenum and cobalt-iron-molybdenum ternary systems at 1200 C
- Hydrodynamic drag of 12- and 21-percent-thick surface-piercing struts
- A flight investigation of laminar and turbulent boundary layers passing through shock waves at full-scale Reynolds numbers
- Investigation of 75-millimeter-bore deep-groove ball bearing under radial load at high speeds 2: oil inlet temperature, viscosity, and generalized cooling correlation
- Investigation at supersonic speeds of the wave drag of seven boattail bodies of revolution designed for minimum wave drag
- Theoretical and measured attenuation of mufflers at room temperature without flow, with comments on engine-exhaust muffler design
- Theoretical calculations of the effects of finite sideslip at supersonic speeds on the span loading and rolling moment for families of thin sweptback tapered wings at an angle of attack
- Theoretical calculation of the pressure distribution, span loading, and rolling moment due to sideslip at supersonic speeds for thin sweptback tapered wings with supersonic trailing edges and wing tips parallel to the axis of wing symmetry
- Use of electric analog for calculation of temperature distribution of cooled turbine blades
- Strength analysis of stiffened thick beam webs with ratios of web depth to web thickness of approximately 60
- Transient temperature distributions in simple conducting bodies steadily heated through a laminar boundary layer
- Theoretical investigation of the longitudinal response characteristics of a swept-wing fighter airplane having a pitch-attitude control system
- The zero-lift drag of a slender body of revolution (NACA RM-10 research model) as determined from tests in several wind tunnels and in flight at supersonic speeds
- Linearized potential theory of propeller induction in a compressible flow
- A linear time-temperature relation for extrapolation of creep and stress-rupture data
- A modified Reynolds analogy for the compressible turbulent boundary layer on a flat plate
- Power-off flare-up tests of a model helicopter rotor in vertical autorotation
- Reaction processes leading to spontaneous ignition of hydrocarbons
- Pressure distributions about finite wedges in bounded and unbounded subsonic streams
- The asymmetric adjustable supersonic nozzle for wind-tunnel application